Accession Number:

AD0653547

Title:

CONCERNING THE PROBLEM OF THE FLOW OF A HYPERSONIC STREAM OF GAS AROUND A THIN BODY,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Monakhov,N. M.

Report Date:

1967-01-23

Pagination or Media Count:

12.0

Abstract:

The hypersonic flow of an ideal gas over slender bodies is discussed. The flow Mach number is assumed to be infinite and is directed along the x-axis. Nondimensional coordinates are introduced, and a boundary value problem is obtained in nondimensional form.

Descriptors:

• (*HYPERSONIC FLOW
• *SLENDER BODIES)
• MACH NUMBER
• BOUNDARY VALUE PROBLEMS
• SHOCK WAVES
• EQUATIONS
• USSR

Subject Categories:

• Aerodynamics
• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE